View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62969U 26145.52192065 +.00000000 +00000-0 +66488-3 0 00008
2 62969 53.1595 235.3832 0001160 87.7530 272.3604 15.30201057 04
| Epoch (UTC): | 25 May 2026 12:31:33 |
| Eccentricity: | 0.0001160 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.3832° |
| argument of perigee: | 87.7530° |
| revolutions per day: | 15.30201057 |
| mean anomaly at epoch: | 272.3604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|